RU2391252C2 - Кожух для летательного аппарата - Google Patents
Кожух для летательного аппарата Download PDFInfo
- Publication number
- RU2391252C2 RU2391252C2 RU2006140524/11A RU2006140524A RU2391252C2 RU 2391252 C2 RU2391252 C2 RU 2391252C2 RU 2006140524/11 A RU2006140524/11 A RU 2006140524/11A RU 2006140524 A RU2006140524 A RU 2006140524A RU 2391252 C2 RU2391252 C2 RU 2391252C2
- Authority
- RU
- Russia
- Prior art keywords
- shell
- stringers
- ribs
- aircraft
- impact
- Prior art date
Links
- 239000004033 plastic Substances 0.000 claims abstract description 9
- 229920003023 plastic Polymers 0.000 claims abstract description 9
- 238000010521 absorption reaction Methods 0.000 claims abstract 3
- 239000000463 material Substances 0.000 claims description 5
- 238000007493 shaping process Methods 0.000 claims description 2
- 238000005452 bending Methods 0.000 claims 1
- 230000003993 interaction Effects 0.000 claims 1
- 230000009466 transformation Effects 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 3
- 239000000126 substance Substances 0.000 abstract 1
- 239000011257 shell material Substances 0.000 description 45
- 229910052751 metal Inorganic materials 0.000 description 11
- 239000002184 metal Substances 0.000 description 11
- 238000003466 welding Methods 0.000 description 5
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 239000004918 carbon fiber reinforced polymer Substances 0.000 description 3
- 238000010276 construction Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- AZDRQVAHHNSJOQ-UHFFFAOYSA-N alumane Chemical group [AlH3] AZDRQVAHHNSJOQ-UHFFFAOYSA-N 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 210000003746 feather Anatomy 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- 238000009827 uniform distribution Methods 0.000 description 1
- 230000004580 weight loss Effects 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/0009—Aerodynamic aspects
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/02—Tailplanes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/04—Noseplanes
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Laminated Bodies (AREA)
- Vibration Dampers (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Air Bags (AREA)
- Finishing Walls (AREA)
- Vehicle Interior And Exterior Ornaments, Soundproofing, And Insulation (AREA)
- Toys (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Devices Affording Protection Of Roads Or Walls For Sound Insulation (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102004018579.4 | 2004-04-16 | ||
DE102004018579A DE102004018579A1 (de) | 2004-04-16 | 2004-04-16 | Verkleidung für eine Struktur eines Flugzeugs |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2006140524A RU2006140524A (ru) | 2008-05-27 |
RU2391252C2 true RU2391252C2 (ru) | 2010-06-10 |
Family
ID=34964732
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2006140524/11A RU2391252C2 (ru) | 2004-04-16 | 2005-04-18 | Кожух для летательного аппарата |
Country Status (10)
Country | Link |
---|---|
US (1) | US20070029443A1 (fr) |
EP (1) | EP1735211B1 (fr) |
JP (1) | JP4699448B2 (fr) |
CN (1) | CN100532196C (fr) |
AT (1) | ATE442292T1 (fr) |
BR (1) | BRPI0509484A (fr) |
CA (1) | CA2560978A1 (fr) |
DE (2) | DE102004018579A1 (fr) |
RU (1) | RU2391252C2 (fr) |
WO (1) | WO2005100152A1 (fr) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ATE441573T1 (de) * | 2003-05-09 | 2009-09-15 | Pilatus Flugzeugwerke Ag | Flugzeugflügel |
US8276847B2 (en) * | 2004-04-16 | 2012-10-02 | Airbus Operations Gmbh | Cover for an aircraft structure |
DE102005060958A1 (de) * | 2005-12-20 | 2007-06-21 | Airbus Deutschland Gmbh | Schutzvorrichtung |
US7766277B2 (en) * | 2006-01-19 | 2010-08-03 | The Boeing Company | Deformable forward pressure bulkhead for an aircraft |
US7997529B2 (en) * | 2006-01-19 | 2011-08-16 | The Boeing Company | Compliant panel for aircraft |
GB0613949D0 (en) * | 2006-07-13 | 2006-08-23 | Airbus Uk Ltd | A wing cover panel assembly and wing cover panel for an aircraft wing and a method of forming thereof |
GB0712552D0 (en) * | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Elongate composite structural members and improvements therein |
GB0807482D0 (en) * | 2008-04-25 | 2008-06-04 | Rolls Royce Plc | Characterisation of soft body impacts |
FR2934562B1 (fr) * | 2008-07-31 | 2011-04-22 | Airbus France | Panneau de protection et module de train d'atterissage le comportant. |
GB0900494D0 (en) * | 2009-01-14 | 2009-02-11 | Airbus Uk Ltd | Aerofoil Structure |
FR2943311B1 (fr) * | 2009-03-19 | 2011-03-04 | Airbus France | Raidisseurs sous bavette pour aeronef |
CN102390520B (zh) * | 2011-09-29 | 2014-06-18 | 西北工业大学 | 一种能够提高飞机抗鸟撞性能的尾翼 |
FR2989666B1 (fr) | 2012-04-19 | 2014-12-05 | Eurocopter France | Surface aerodynamique portante d'aeronef, et aeronef muni de ladite surface aerodynamique portante |
US10437742B2 (en) * | 2014-10-10 | 2019-10-08 | Microsoft Technology Licensing, Llc | Vendor-specific peripheral device class identifiers |
JP6782533B2 (ja) | 2015-08-26 | 2020-11-11 | 三菱航空機株式会社 | 航空機の前縁構造体、航空機の翼及び航空機 |
CN106697258B (zh) * | 2016-11-28 | 2019-05-10 | 西北工业大学 | 一种能够提高飞机抗鸟撞性能的机翼前缘 |
GB201821332D0 (en) * | 2018-12-31 | 2019-02-13 | Airbus Operations Gmbh | Aircraft flow body |
EP3683139B1 (fr) * | 2019-01-18 | 2021-07-28 | Airbus Operations, S.L.U. | Surface de commande de vol pour aéronef et procédé de fabrication dudit de surface de commande de vol |
CN110304237B (zh) * | 2019-07-15 | 2023-08-25 | 中国商用飞机有限责任公司 | 飞行器机翼及包括该飞行器机翼的飞行器 |
RU199992U1 (ru) * | 2020-06-26 | 2020-10-01 | Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации | Клиновидный радиопрозрачный передний обтекатель корпуса сверхзвукового летательного аппарата |
Family Cites Families (35)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1939599A (en) * | 1931-08-13 | 1933-12-12 | Budd Edward G Mfg Co | Aerofoil beam |
US2367750A (en) * | 1941-01-17 | 1945-01-23 | Central Aircraft Corp | Aircraft construction |
US2390761A (en) * | 1943-06-16 | 1945-12-11 | Budd Edward G Mfg Co | Aircraft structure |
US2407614A (en) * | 1943-07-03 | 1946-09-10 | Budd Co | Structure for supporting fuel tanks in aircraft wings |
US2427853A (en) * | 1944-02-23 | 1947-09-23 | Curtiss Wright Corp | Aircraft construction |
US2567124A (en) * | 1946-05-10 | 1951-09-04 | Curtiss Wright Corp | Airfoil construction |
US2742247A (en) * | 1950-10-31 | 1956-04-17 | Handley Page Ltd | Outer surfaces for craft moving in one fluid |
US3976269A (en) * | 1974-12-19 | 1976-08-24 | The Boeing Company | Intrinsically tuned structural panel |
US4148450A (en) * | 1975-05-06 | 1979-04-10 | Hermann Neuhierl | Model aircraft construction |
US4171785A (en) * | 1977-06-30 | 1979-10-23 | The Boeing Company | Apparatus and method for manufacturing laminar flow control aircraft structure |
US4356616A (en) * | 1980-02-25 | 1982-11-02 | Rockwell International Corporation | Method of making rib structures for an airfoil |
US4481703A (en) * | 1980-02-25 | 1984-11-13 | Rockwell International Corporation | Method of making rib structures for an airfoil |
US4739954A (en) * | 1986-12-29 | 1988-04-26 | Hamilton Terry W | Over-lap rib joint |
US5242523A (en) * | 1992-05-14 | 1993-09-07 | The Boeing Company | Caul and method for bonding and curing intricate composite structures |
US5560102A (en) * | 1992-10-13 | 1996-10-01 | The Boeing Company | Panel and fuselage assembly |
DE4315600C2 (de) * | 1993-05-11 | 1996-07-25 | Daimler Benz Aerospace Airbus | Tragstruktur für eine aerodynamische Fläche |
DE69733941T2 (de) * | 1996-03-22 | 2006-06-14 | Boeing Co | Bestimmter flügelaufbau |
US5744197A (en) * | 1996-08-26 | 1998-04-28 | J. B. Faith Co. | Method of protecting aluminum skins of land vehicles from corrosion |
US6766984B1 (en) * | 1998-07-16 | 2004-07-27 | Icom Engineering Corporation | Stiffeners for aircraft structural panels |
DE19844035C1 (de) * | 1998-09-25 | 1999-11-25 | Daimler Chrysler Aerospace | Schalenbauteil für ein Flugzeug und Verfahren zur Herstellung |
US6116268A (en) * | 1998-11-17 | 2000-09-12 | Barber Industries Inc. | Wellhead safety valve control system |
DE10005348B4 (de) * | 2000-02-08 | 2004-05-06 | Airbus Deutschland Gmbh | Verfahren zur Fertigung von Nasenstrukturen für aerodynamische Flächen |
DE10007995C2 (de) * | 2000-02-22 | 2002-03-07 | Airbus Gmbh | Strukturbauteil, insbesondere für ein Flugzeug und Verfahren zur Herstellung eines Strukturbauteils |
DE10031510A1 (de) * | 2000-06-28 | 2002-01-17 | Airbus Gmbh | Strukturbauteil für ein Flugzeug |
ES2197727B1 (es) * | 2000-07-27 | 2005-04-01 | Construcciones Aeronauticas, S.A. | Borde de ataque de superficies sustentadoras de aeronaves. |
US6712315B2 (en) * | 2000-11-30 | 2004-03-30 | Airbus Deutschland Gmbh | Metal structural component for an aircraft, with resistance to crack propagation |
JP4526698B2 (ja) * | 2000-12-22 | 2010-08-18 | 富士重工業株式会社 | 複合材成形品及びその製造方法 |
SE517133C2 (sv) * | 2001-06-05 | 2002-04-16 | Saab Ab | Anordning för att stödja en skalyta i ett flygplansskrov |
SE519185C2 (sv) * | 2001-06-07 | 2003-01-28 | Saab Ab | Flygplanspanel |
DE10129576B4 (de) * | 2001-06-20 | 2005-06-02 | Fairchild Dornier Gmbh | Strukturelement für ein Luftfahrzeug |
JP4574086B2 (ja) * | 2001-09-03 | 2010-11-04 | 富士重工業株式会社 | 複合材翼の製造方法および複合材翼 |
US6648273B2 (en) * | 2001-10-30 | 2003-11-18 | The Boeing Company | Light weight and high strength fuselage |
JP2004025946A (ja) * | 2002-06-24 | 2004-01-29 | Honda Motor Co Ltd | 航空機の翼構造 |
US20040035979A1 (en) * | 2002-08-23 | 2004-02-26 | Mccoskey William Robert | Integrally stiffened axial load carrying skin panels for primary aircraft structure and closed loop manufacturing methods for making the same |
US7159822B2 (en) * | 2004-04-06 | 2007-01-09 | The Boeing Company | Structural panels for use in aircraft fuselages and other structures |
-
2004
- 2004-04-16 DE DE102004018579A patent/DE102004018579A1/de not_active Withdrawn
-
2005
- 2005-04-18 BR BRPI0509484-4A patent/BRPI0509484A/pt not_active IP Right Cessation
- 2005-04-18 CN CNB2005800114105A patent/CN100532196C/zh not_active Expired - Fee Related
- 2005-04-18 EP EP05733257A patent/EP1735211B1/fr not_active Not-in-force
- 2005-04-18 DE DE502005008106T patent/DE502005008106D1/de active Active
- 2005-04-18 RU RU2006140524/11A patent/RU2391252C2/ru not_active IP Right Cessation
- 2005-04-18 CA CA002560978A patent/CA2560978A1/fr not_active Abandoned
- 2005-04-18 AT AT05733257T patent/ATE442292T1/de not_active IP Right Cessation
- 2005-04-18 WO PCT/EP2005/004097 patent/WO2005100152A1/fr active Application Filing
- 2005-04-18 JP JP2007507775A patent/JP4699448B2/ja not_active Expired - Fee Related
-
2006
- 2006-10-16 US US11/581,543 patent/US20070029443A1/en not_active Abandoned
Non-Patent Citations (1)
Title |
---|
Житомирский Г.И. Конструкция самолетов. - М.: Машиностроение, 1991, рис.2.62, 2.63, с.87-90. * |
Also Published As
Publication number | Publication date |
---|---|
JP4699448B2 (ja) | 2011-06-08 |
JP2007532397A (ja) | 2007-11-15 |
CN1942363A (zh) | 2007-04-04 |
CA2560978A1 (fr) | 2005-10-27 |
EP1735211B1 (fr) | 2009-09-09 |
EP1735211A1 (fr) | 2006-12-27 |
DE102004018579A1 (de) | 2005-11-03 |
BRPI0509484A (pt) | 2007-09-11 |
CN100532196C (zh) | 2009-08-26 |
DE502005008106D1 (de) | 2009-10-22 |
RU2006140524A (ru) | 2008-05-27 |
WO2005100152A1 (fr) | 2005-10-27 |
ATE442292T1 (de) | 2009-09-15 |
US20070029443A1 (en) | 2007-02-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PD4A | Correction of name of patent owner | ||
MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20170419 |